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Research Articles

Influences of injection parameters on performance of blockerless thrust reverser

  • ZHANG Yun-Hao ,
  • Eriqitai
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  • Beijing University of Aeronautics and Astronautics, Beijing 100191,China

Received date: 2011-01-28

  Revised date: 2011-03-07

  Online published: 2011-05-15

Abstract

By using CFD technology, the flow field of a blockerless thrust reverser experiment model with the bypass ratio of 9 was simulated. Variations in reverser efficiency, cascade flow ratio, and the injection flow ratio with the injection parameter was described. Based on detailed analysis of the thrust reverser flow characteristics, we found that the location of secondary injection, slot angle, and slot width have great impacts on the performance of thrust reversers. The optimum value of injection parameter can then be obtained.

Cite this article

ZHANG Yun-Hao , Eriqitai . Influences of injection parameters on performance of blockerless thrust reverser[J]. Journal of University of Chinese Academy of Sciences, 2011 , 28(3) : 298 -303 . DOI: 10.7523/j.issn.2095-6134.2011.3.003

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